[olegmang]

Hi guys. As I see this topic is still being viewed, but mainly for the geometry. Several people have already asked me about it so I decided to update the link. Here is the fresh link to my google drive.
https://drive.google.com/folderview?...0k&usp=sharing

Hope this'll help. Good luck!

[gusano154]

Thanks, olegmang!

[manjunathdc014]

Hi
I am working on subsonic axial compressor stage 37 (rotor and stator) turbo-grid curves files.i have the data of stage 37 blade coordinates,i have rotor 37 blade coordinates.csv file of hub,shroud and blade profile and its matching no of blades in rotor is 36
currently i am facing problem in stator turbo-grid coordinates.i am unable to create hub.curve,shroud.curve and blade profile .curve,
if anyone having turbogrid curve files for stage pls send it,no of blade in stator is 46,
journal which i am working
Design and Overall Performance
of Four Highly Loaded, High-Speed
Inlet Stages for an Advanced
High-Pressure-Ratio Core Compressor,Lonnie Reid and Royce D. Moore
Lewis Research Center
Cleveland, Ohio stage page 44-51,stage 37,

[manjunathdc014]

Hi friends,i have done stage 37 mesh using turbogrid,
mesh of stator is fine,but when i use rotor 37 .i am getting -ve volume.can you guys pls send me the mesh file of rotor and stator 37.
i.e gtm file

[mohammadest]

Dear all
I need the geometry of NASA axial compressor stage 36 & 38 , If you have stage36 or38 geometry's data, wish u could share them with me

geometry cad file or geometry excel file.

i have a problem in geometry of both them.when i draw stage 36 & 38 ,some sketch look wrong.but i dont know why.

please help me.

email : mohammad_est@yahoo.com

[zgeorgak]

Originally Posted by olegmang

In fact, I have coordinates in more convenient format for you (see attached). I've already extracted them from turbogrids rotor for each section and put into separate .txt files that you can easily import to SolidWorks and then loft a surface.

Hello. I know it's been a while since this thread was active, but could you tell me how you moved from turbogrid back to profile across the blade's span please? Thanks

[Sidhartha24]

I am trying to simulate transonic flow on NASA rotor 37. Can someone help me with the geometry?

Thank you.

[QINK]

[QUOTE=manjunathdc014;578602]Hi brother
I am working on subsonic axial compressor stage 37 (rotor and stator) turbo-grid curves files too.I have the curve data and the mesh of the rotor,but i don't
have that of the stator. If you still have the data, could you please provide me with one,what's more ,IF you need the mesh(file:Rotor37.cfx,Rotor37.def) of the rotor,I CAN offer you mine.My mail:2393444190qin@gmail.com
thank you sososo much
respect

[Mozakker]

I'm a beginner . my professor asked me to make a model of NASA stage 37 using ANSYS. Can anyone help me with this model please
my mail : shojibhosen173@gmail.com

[ghorrocks]

Please refer to the FAQ on how to ask questions on the forum: https://www.cfd-online.com/Wiki/Ansy...ible_answer.3F

[oussamae]

Originally Posted by olegmang

Hi guys. As I see this topic is still being viewed, but mainly for the geometry. Several people have already asked me about it so I decided to update the link. Here is the fresh link to my google drive.
https://drive.google.com/folderview?...0k&usp=sharing

Hope this'll help. Good luck!

can you please update the link?